This paper presents the development of indigenous hybrid rocket technology, using 98%
hydrogen peroxide as an oxidizer. Consecutive steps are presented, which started with …

This paper discusses the potential use of hydrogen peroxide as oxidizer for solid rocket
propulsion. While hydrogen peroxide is a liquid in normal conditions, it may be used in solid …

Two different diameters of Pt/Al 2 O 3 spherical catalysts (1 mm and 2 mm) for HTP 98%
decomposition were tested to compare the catalytic activity and catalyst ageing. Comparable …

This paper presents a comprehensive review of the physical and chemical properties of
hydrogen peroxide as well as some regularities of its decomposition in the liquid phase …

(17) Lukasiewicz Research Network–Institute of Aviation, Center of Unmanned
Technologies, Warsaw, Poland. michal. kawalec@ ilot. lukasiewicz. gov. pl (18) Lukasiewicz …

The use of different diameters of Pt/Al2O3 spherical catalysts for HTP 98% decomposition (1
mm and 2 mm) enabled a better reactivity of the decomposition process for the smaller one …

Numerical analysis can be used to optimise design of the green propulsion thruster with
competitive costs compared to optimisation process through experiments. Furthermore, it …

Liquid fuel combustion with catalytically decomposed hydrogen peroxide hot stream for
bipropellant thruster application has been studied in PPrime's combustion facility ACSEL. An …

In Europe, but also in many other countries initiative to replace toxic and corrosive rocket
propellants based on hydrazine fuels and nitrogen tetroxide oxidizers with green propellants …